Garmin 0194500 Users Manual
GIA 63
DRAFT
Installation Manual
190-00303-05 November, 2012 Revision W
© Copyright 2012
DRAFT
Garmin Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or
stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium
to be viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or printed copy of this
manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial
distribution of this manual or any revision hereto is strictly prohibited.
Garmin International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
Aviation Dealer Technical Support Line (Toll Free): (888) 606-5482
www.garmin.com
Garmin (Europe) Ltd
Liberty House
Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, UK
Telephone: +44 (0) 8708501241
RECORD OF REVISIONS
Revision
A 11/15/04 Production Release
B 3/16/05 Updated pinout list, removed EQF and ETSO 2C37e deviation
C 6/23/05 Added additional interconnects, TSO-C9c, and TSO-C52b
D 10/26/05 Added TSO-C151b and boot block instructions
E 6/8/06 Edited document to include the GIA 63W
F 7/21/06 Corrected WAAS TSO
G 9/19/06 Added RTCA/DO-229C deviation
H 10/18/06 Added Comant antennas
J 4/10/07 Added Comant antenna and revised ICAW
K 6/6/07 Added the 011-01105-01 unit
L 8/23/07 Changed operational limitations and added antennas
M 2/29/08 Added ETSO information
N 5/27/09 Added TSO-C92c and other TSO info
P 9/09/09 Added Level A CLD information
Q 12/29/09 Added antenna note
R 3/23/10 Added standalone rack info
S 7/29/10 Added updated NAV/COM unit
T 11/24/10 Added GIA 63H model info, changed doc title
U 12/27/11 Added GIA 63W and 63H ETSOs
V 8/23/12 Added TSO-C54
W 11/12/12 Added -40 GIA 63W
Revision
Date
Description
190-00303-05 GIA 63 Installation Manual
Rev. W Page A
CURRENT REVISION DESCRIPTION
DRAFT
Revision
W
Page
Number(s)
1-3 1.4.2 Specified unit and connector weights
1-6 1.4.6 Specified squelch specifications
1-9 1.4.10 Specified power requirements
1-10 1.4.11 Added -40 unit, edited RTCA reference, and added note
1-11 1.5 Specified emission type for each unit
1-12 1.6
1-34 - 1-39 1.6.8 & 1.6.9 Added -40 TSOs and TSO deviations
1-41 - 1-43 1.6.10.2 Added TSOs and edited AC references
1-46 1.6.12 Specified regulatory specs by unit
1-47 1.7 Added GDR 66 Installation Manual reference
2-1 2.1.1 Added -40 unit
2-2 2.1.2 Added IF Seal kit
2-3 2.1.3 Added TSOs and specified units
2-3 2.1.3.2
2-6 2.2.1 Standardized antenna wording
2-9 2.2.3 Clarified Com antenna location wording
2-13 2.7 Added TSO
2-14 2.8.1 Added Mounting Limitations section
3-6 3.8 Edited RTCA reference and added -40 unit
4-1 - 4-5 4 Added -40 pins
4-24 4.6.1 Specified functions based on unit and software
4-25 - 4-27 4.6.2.3 - 4.6.2.5 Clarified spec descriptions and added -40 pins
4-28 - 4-30 4.7.1 - 4.7.2.7 Added -40 pins
Section
Number
Description of Change
Replaced “WAAS” with “LNAV/VNAV, LP, and LPV” and added
software specific paragraph
Clarified software version and corrected section
reference
DOCUMENT PAGINATION
Section Page Range
Table of Contents i – viii
Section 1 1-1 – 1-48
Section 2 2-1 – 2-18
Section 3 3-1 – 3-8
Section 4 4-1 – 4-40
Section 5 5-1 – 5-6
Appendix A A-1 – A-4
Appendix B B-1 – B-6
Appendix C C-1 – C-7
190-00303-05 GIA 63 Installation Manual
Rev. W Page i
INFORMATION SUBJECT TO EXPORT CONTROL LAWS
DRAFT
This document may contain information which is subject to the Export Administration
Regulations (“EAR”) issued by the United States Department of Commerce (15 CFR,
Chapter VII Subchapter C) and which may not be exported, released or disclosed to
foreign nationals inside or outside the United States without first obtaining an export
license. The preceding statement is required to be included on any and all reproductions
in whole or in part of this manual.
GIA 63 Installation Manual 190-00303-05
Page ii Rev. W
Limited Warranty
DRAFT
All Garmin avionics products are warranted to be free from defects in materials or workmanship for: two years from the date of
purchase for new Remote-Mount and Panel-Mount products; one year from the date of purchase for new portable products and any
purchased newly-overhauled products; six months for newly-overhauled products exchanged through a Garmin Authorized
Service Center; and 90 days for factory repaired or newly-overhauled products exchanged at Garmin in lieu of repair. Within the
applicable period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or
replacement will be made at no charge to the customer for parts or labor, provided that the customer shall be responsible for any
transportation cost. This warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts,
such as batteries, unless product damage has occurred due to a defect in materials or workmanship; (iii) damage caused by
accident, abuse, misuse, water, flood, fire, or other acts of nature or external causes; (iv) damage caused by service performed by
anyone who is not an authorized service provider of Garmin; or (v) damage to a product that has been modified or altered without
the written permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims against products or services that
are obtained and/or used in contravention of the laws of any country.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER
WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER
ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR
OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL
DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR FROM
DEFECTS IN THE PRODUCT. SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR
CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or
software or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND
EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
Online Auction Purchases: Products purchased through online auctions are not eligible for warranty coverage. Online auction
confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from
the original retailer is required. Garmin will not replace missing components from any package purchased through an online
auction.
International Purchases: A separate warranty may be provided by international distributors for devices purchased outside the
United States depending on the country. If applicable, this warranty is provided by the local in-country distributor and this
distributor provides local service for your device. Distributor warranties are only valid in the area of intended distribution. Devices
purchased in the United States or Canada must be returned to the Garmin service center in the United Kingdom, the United States,
Canada, or
Garmin International, Inc. Garmin (Europe) Ltd.
1200 E. 151st Street Liberty House
Olathe, KS 66062, U.S.A. Bulls Copse Road
Phone: 800/800.1020 Hounsdown Business Park
FAX: 913/397.0836 Southampton, SO40 9RB, UK
Taiwan for service.
Telephone: 44 (0) 8708501241
190-00303-05 GIA 63 Installation Manual
Rev. W Page iii
1 GENERAL DESCRIPTION ...........................................................................1-1
DRAFT
1.1 Introduction .....................................................................................................................1-1
1.2 Equipment Description....................................................................................................1-1
1.3 Interface Summary .......................................................................................................... 1-2
1.4 Technical Specifications.................................................................................................. 1-3
1.5 License Requirements.................................................................................................... 1-11
1.6 Certification...................................................................................................................1-12
1.7 Reference Documents.................................................................................................... 1-47
2 INSTALLATION OVERVIEW......................................................................2-1
2.1 Introduction .....................................................................................................................2-1
2.2 Installation Considerations.............................................................................................. 2-6
2.3 Rack Considerations......................................................................................................2-10
2.4 Cabling and Wiring .......................................................................................................2-11
2.5 Cooling Air....................................................................................................................2-11
2.6 GIA 63 Minimum Installation Requirements................................................................ 2-12
2.7 GIA 63W and GIA 63H Minimum Installation Requirements ..................................... 2-13
2.8 Mounting Requirements................................................................................................ 2-14
3 INSTALLATION PROCEDURE...................................................................3-1
3.1 Unpacking Unit................................................................................................................ 3-1
3.2 Wiring Harness Installation.............................................................................................3-2
3.3 Antenna Installation......................................................................................................... 3-3
3.4 Cable Installation............................................................................................................. 3-3
3.5 Backshell Assembly ........................................................................................................3-4
3.6 Unit Installation...............................................................................................................3-4
3.7 Post Installation Configuration & Checkout ...................................................................3-5
3.8 Continued Airworthiness................................................................................................. 3-6
4 SYSTEM INTERCONNECTS........................................................................4-1
4.1 Pin Function List .............................................................................................................4-1
4.2 Power and Antennas......................................................................................................4-17
4.3 GIA System ID Program ............................................................................................... 4-19
4.4 Serial Data ..................................................................................................................... 4-19
4.5 Discrete I/O.................................................................................................................... 4-23
4.6 COM/VOR/ILS/Digital Audio...................................................................................... 4-24
4.7 VOR/ILS Indicator ........................................................................................................ 4-28
4.8 RMI/OBI........................................................................................................................ 4-32
4.9 DME Tuning and ADF..................................................................................................4-33
4.10 Auto Pilot..................................................................................................................... 4-35
GIA 63 Installation Manual 190-00303-05
Page iv Rev. W
Appendix A GIA 63 MAIN BOOT BLOCK UPLOADING INSTRUCTIONS.....A-1
DRAFT
A.1 Introduction.................................................................................................................... A-1
A.2 Determining Current Boot Block................................................................................... A-1
A.3 Loading Boot Block Version 4.01.................................................................................A-2
A.4 Loading GIA Main Software (only if GIA main software was cancelled in Section A.2)A-3
Appendix B OUTLINE AND INSTALLATION DRAWINGS................................B-1
Appendix C INTERCONNECT DRAWINGS...........................................................C-1
190-00303-05 GIA 63 Installation Manual
Rev. W Page v
GIA 63 HARDWARE MOD LEVEL HISTORY
DRAFT
The following table identifies hardware modification (Mod) Levels for the GIA 63. Mod Levels are listed
with the associated service bulletin number, service bulletin date, and the purpose of the modification.
The table is current at the time of publication of this manual (see date on front cover) and is subject to
change without notice. Authorized Garmin Sales and Service Centers are encouraged to access the most
up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at
www.garmin.com using their Garmin-provided user name and password.
GIA 63 P/N 011-00781-00, 011-00781-01 HARDWARE MOD LEVEL HISTORY
APPLICABLE
LRU PART
NUMBER
011-00781-00
011-00781-01 1 N/A N/A
MOD
LEVEL
1 0416 9/13/2004
2 0418 9/8/2004
3 0505 1/19/2005
4N/A N/A
SERVICE
BULLETIN
NUMBER
SERVICE
BULLETIN
DATE
PURPOSE OF
MODIFICATION
This modification consists of
modifying the voice alert audio
output circuit, enabling it to power
down when not in use.
This Service Bulletin consists of
visually inspecting the GIA 63 Main2
board for incorrectly installed
capacitors.
This modification addresses a
potential GIA 63 COM transceiver
interference condition.
More robust capacitors installed in
the power supply backup circuit.
More robust capacitors installed in
the power supply backup circuit.
GIA 63 Installation Manual 190-00303-05
Page vi Rev. W
GIA 63W/GIA 63H HARDWARE MOD LEVEL HISTORY
DRAFT
The following table identifies hardware modification (Mod) Levels for the GIA 63W and GIA 63H. Mod
Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the
modification. The table is current at the time of publication of this manual (see date on front cover) and is
subject to change without notice. Authorized Garmin Sales and Service Centers are encouraged to access
the most up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at
www.garmin.com using their Garmin-provided user name and password.
GIA 63W/GIA 63H P/N 011-01105-XX HARDWARE MOD LEVEL HISTORY
APPLICABLE
LRU PART
NUMBER
011-01105-00 1 N/A N/A
011-01105-01 N/A N/A N/A N/A
011-01105-20 N/A N/A N/A N/A
011-01105-30 N/A N/A N/A N/A
MOD
LEVEL
SERVICE
BULLETIN
NUMBER
SERVICE
BULLETIN
DATE
PURPOSE OF
MODIFICATION
More robust capacitors installed in
the power supply backup circuit.
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DRAFT
GIA 63 Installation Manual 190-00303-05
Page viii Rev. W
1 GENERAL DESCRIPTION
NOTE
CAUTION
DRAFT
1.1 Introduction
This manual is intended to provide mechanical and electrical information for use in the planning and
design of an installation of the GIA 63(X) into an aircraft. This manual is not a substitute for an approved
airframe-specific maintenance manual, installation design drawing, or complete installation data package.
Attempting to install equipment by reference to this manual alone and without first planning or designing
an installation specific to your aircraft may compromise your safety and is not recommended. The content
of this manual assumes use by competent and qualified avionics engineering personnel and/or avionics
installation specialists using standard aviation maintenance practices in accordance with Title 14 of the
Code of Federal Regulations and other relevant accepted practices. This manual is not intended for use by
individuals who do not possess the competencies and abilities set forth above.
Garmin recommends installation of the GIA 63(X) by a Garmin-authorized installer. To
the extent allowable by law, Garmin will not be liable for damages resulting from
improper or negligent installation of the GIA 63(X). For questions, please contact Garmin
Aviation Product Support at 1-888-606-5482.
1.2 Equipment Description
The GIA 63(X) is a microprocessor-based input/output Line Replaceable Unit (LRU) used in a Garmin
Integrated Flight Deck. The GIA 63(X) communicates with the GDU via Ethernet high-speed data bus
(HSDB), and with other LRUs using RS-232, RS-485/422, and ARINC 429. All configuration is done
through the GDU. The GIA 63(X) contains the following sub-assemblies:
• A main processor that interfaces with all LRUs in the G1000 sub-system and performs calculations
for the GFC 700 autopilot (if equipped).
• A twelve channel parallel GPS receiver that simultaneously tracks and uses up to 12 satellites. The
GIA 63W and GIA 63H include a 15 channel WAAS certified GPS receiver.
• A VHF COM transceiver that provides tuning from 1 18. 00 to 136.992 MHz in 25 kHz or 8.33 kHz
spacing for 760 or 2280 channel configuration respectively.
• A VOR/ILS localizer receiver that provides tuning from 108.00 to 117.95 MHz in 50 kHz
increments.
• An ILS glideslope receiver that provides tuning from 328.6 to 335.4 MHz as paired with the
frequency tuned on the VOR/ILS localizer receiver.
The operation of unapproved cellular telephones or other unapproved cellular devices aboard
aircraft while airborne is prohibited by FCC rules. Due to the potential for interference with
onboard systems, the operation of unapproved cellular communication devices while onboard an
aircraft that is on the ground is subject to FAA regulations 14 CFR 91.21.
FCC regulation 47 CFR 22.925 prohibits airborne operation of unapproved cellular telephones
installed in or carried aboard aircraft. Unapproved cellular telephones must not be operated
aboard any aircraft while the aircraft is off the ground. When any aircraft leaves the ground, all
unapproved cellular telephones on board that aircraft must be turned off.
Unapproved cellular telephones that are on, even in a monitoring state, can disrupt GPS
performance.
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-1
1.3 Interface Summary
DRAFT
1.3.1 Primary Interfaces
The GIA 63(X) is designed as an open architecture system that provides the following interfaces:
• 1 dedicated Ethernet High-Speed Data Bus (HSDB) input/output channel
• 2 Controller Area Network (CAN) I/O channels
• 8 Main ARINC 429 inputs
• 3 Main ARINC 429 outputs
• 1 VOR/ILS ARINC 429 input
• 1 VOR/ILS ARINC 429 output
• 5 RS-485 input/output channels (any two RS-485 channels can be configured to form a single
RS-422 channel)
• 8 RS-232 input/output channels
• 41 Discrete inputs
• 14 Discrete outputs
• 24 Annunciator outputs
1.3.2 Additional Interfaces
The GIA 63(X) can provide interfaces for the following additional equipment:
• Autopilot
• Altitude encoder/serializer
• Fuel management systems
• Lightning detection systems
• Traffic awareness systems
• Data link systems
• External annunciators
• DME (including King Serial)
• ADF
GIA 63 Installation Manual 190-00303-05
Page 1-2 Rev. W
1.4 Technical Specifications
DRAFT
1.4.1 Environmental Qualification Form
It is the responsibility of the installing agency to obtain the latest revision of the GIA 63(X) Environmental
Qualification Form. This form is available directly from Garmin under the following part number:
GIA 63 Environmental Qualification Form, Garmin part number 005-00148-02
GIA 63W Environmental Qualification Form, Garmin part number 00 5-00235-00
The GIA 63H and the GIA 63W are included in the 005-00235-00. To obtain a copy of this form, see the
dealer/OEM portion of the Garmin web site (www.garmin.com).
1.4.2 Physical Characteristics
Table 1-1. GIA 63(X) Physical Characteristics
Characteristic Specification
Modular Rack Width 3.83 inches (97.3 mm)
Modular Rack Height 7.26 inches (184.4 mm)
Standalone Rack Width 3.88 inches (98.5 mm)
Standalone Rack Height 6.91 inches (175.5 mm)
Depth w/connectors (Modular and Standalone) 10.20 inches (259.1 mm)
011-00781-0X: 5.3 lbs. (2.40 kg)
Unit Weight
Modular Rack Weight w/Back Plate 1.0 lbs. (0.45 kg)
Standalone Rack Weight w/Back Plate 1.3 lbs. (0.59 kg)
Helicopter Rack Width 3.76 inches (95.4 mm)
Helicopter Rack Height 7.00 inches (177.8 mm)
Depth w/connectors (Helicopter) 10.18 inches (258.6 mm)
Unit Weight (Helicopter) 011-01105-3X: 5.4 lbs (2.45 kg)
Helicopter Rack Weight w/Back Plate 1.6 lbs (0.74 kg)
Connector Kit Weight*
* Only the GIA 63H unit (011-01105-3X) together with the Helicopter Rack (011-02425-00), Back Plate (011-00963-01), and Connector Kit
(011-01000-01) is approved for DO-160F, Category U, Curve G vibration levels.
011-01105-0X/-1X/-2X: 5.3 lbs. (2.40 kg)
011-01105-4X: 5.5 lbs. (2.49 kg)
011-01000-00: 1.3 lbs (0.59 kg)
011-01000-01: 1.1 lbs (0.50 kg)
011-01000-03: 1.1 lbs (0.50 kg)
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-3
1.4.3 General Specifications
DRAFT
For detailed specifications, see the Environmental Qualification Form.
Table 1-2. GIA 63(X) General Specifications
Characteristic Specification
Operating Temperature Range
Humidity 95% non-condensing
Altitude Range -1,500 ft to 50,000 ft
-40°C to +65°C. For more details see Environmental
Qualification Form
GIA 63 Installation Manual 190-00303-05
Page 1-4 Rev. W
1.4.4 GPS Specification (GIA 63 only)
DRAFT
Table 1-3. GIA 63 GPS Specifications
Characteristic Specification
a) Search-the-Sky (without almanac, without initial position or
time): 5 minutes
b) AutoLocate™ (with almanac, without initial position or
Acquisition Times
Max Velocity 1000 knots
Dynamics 6g
Antenna power supply 20 mA typical, 40 mA max at 4.6 VDC
1.4.5 WAAS Specific GPS Specifications (GIA 63W & GIA 63H)
time): 5 minutes
c) Cold Start (position known to 300 nm, time known to 10 minutes,
with valid almanac): 45 seconds
d) Warm Start (position known to 10 nm, time known to 10 minutes,
with valid almanac and ephemeris): 15 seconds
Table 1-4. GIA 63W and GIA 63H GPS Specifications
Characteristic Specification
Number of channels 15 (12 GPS and 3 GPS/WAAS/SBAS)
Frequency 1575.42 MHz L1, C/A code
Sensitivity
(acquisition)
Sensitivity
(drop lock)
Lat/Long position
accuracy
Velocity 1000 knots maximum (above 60,000 ft)
TTFF (time to first fix) 1:45 min. typical with current almanac, position, and tim
Reacquisition 10 seconds typical for signal outages of 30 seconds or less
Position update
interval
1 pps (pulse per
second)
Datum WGS-84
SATCOM
compatibility
-116 dBm to -134.5 dBm GPS
-116 dBm to -134.5 dBm WAAS
-144 dBm
<1.25 meter RMS horizontal, <2 meter vertical, with WAAS
0.2 sec (5 Hz)
±275 nsec of UTC second during steady-state navigation
Compatible on aircraft equipped with SATCOM (see Section
2.1.3.2 for SATCOM compatible antennas)
Antenna power supply
at GPS port
190-00303-05 GIA 63 Installation Manual
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4.3 VDC to 4.8 VDC @ 60 mA
1.4.6 COM Transceiver Specifications
DRAFT
Table 1-5. GIA 63(X) COM Transceiver Specifications
Characteristic Specification
Audio Output 100 mW minimum into a 500 Ω load
Audio Response Less than 6 dB of variation between 350 and 2500 Hz
Audio Distortion
AGC Characteristics
Sensitivity
25 kHz Channel
Squelch
8.33 kHz Channel
Squelch
Selectivity
Spurious Response Greater than 80 dB
The distortion in the receiver audio output shall not exceed 25% at all levels
up to 100 mW
The audio output shall not vary by more than 6 dB when the level of the RF
input signal, modulated 30% at 1000 Hz, is varied from 5 μV to 100,000 μV
(hard)
(S+N)/N on all channels shall be greater than 6 dB when the RF level is 2 μV
(hard) modulated 30% at 1000 Hz at rated audio
2 μv (hard) ±6 dB
011-00781-0X and 011-01105-0X:
3 μv (hard) ±6 dB
011-01105-2X/-3X/-4X:
2 μv (hard) ±6 dB
6 dB BW is greater than ±8 kHz for 25 kHz channeling
60 dB BW is less than ±25 kHz for 25 kHz channeling
6 dB BW is greater than ±2.778 kHz for 8.33 kHz channeling
60 dB BW is less than ±7.37 kHz for 8.33 kHz channeling
At Least 16 watts when Vin = 28 VDC
Transmitter Power
Transmitter Duty Cycle Recommended 10% maximum
Modulation Capability*
Carrier Noise Level Shall be at least 45 dB (S+N)/N
Frequency Stability 0.0005%
Demodulated Audio
Distortion
Sidetone 1.4 VRMS into a 500 Ω load when the transmitter is modulated at least 70%
Demodulated Audio
Response
*When utilizing the configurable microphone gain adjustments, the modulation capability specification can be met with a 70 mVrms to 3.0 Vrms
analog microphone input signal applied to the transmitter. When a digital audio microphone signa l is provided by a compatible Garmin audio panel,
the modulation capability specification can be met with a minimum 70 mVrms microphone input signal applied to the audio panel.
GIA 63 Installation Manual 190-00303-05
Page 1-6 Rev. W
At least 10 watts when Vin = 14 VDC (011-01105-2X and 011-01105-3X
only)
The modulation shall not be less than 70% and not greater than 99.9% with
a standard modulator signal applied to the transmitter
Less than 10% distortion when the transmitter is modulated at least 70%
Shall be less than 6 dB when the audio input frequency is varied from 350 to
2500 Hz
1.4.7 VOR Specifications
DRAFT
Table 1-6. GIA 63(X) VOR Specifications
Characteristic Specification
Receiver Audio
Sensitivity
Course Deviation
Sensitivity
Flag
AGC Characteristics
Spurious Response Greater than 60 dB
VOR OBS Bearing
Accuracy
Audio Output A minimum 100 mW into a 500 Ω load
Audio Response
At -103.5 dBm (S+N)/N shall not be less than 6 dB
At –103.5 dBm deviation output shall not be less than 60% of standard
deflection (90 mV) when a VOR deviation test signal is applied (10 degrees
course difference)
The VLOC Course Deviation Flag must be flagged:
a) in the absence of an RF signal
b) in the absence of the 9960 Hz modulation
c) in the absence of either one of the two 30 Hz modulations
d) When the level of a standard VOR deviation test signal produces less
than a 50% of standard deflection
From -99 dBm to -13 dBm input of a Standard VOR Audi o Test Signal, audio
output levels shall not vary more than 3 dB
The bearing information as presented to the pilot shall not have an error in
excess of 2.7° as specified by RTCA DO-196 and EuroCAE ED-22B
Less than 6 dB of variation between 350 and 2500 Hz. In voice mode, an
ident tone of 1020 Hz shall be attenuated at least 20 dB
Audio Distortion
Selectivity 6 dB BW is greater than 16.5 kHz
The distortion in the receiver audio output shall not exceed 10% at all levels
up to 100 mW
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1.4.8 LOC Specifications
DRAFT
Table 1-7. GIA 63(X) LOC Specifications
Characteristic Specification
Receiver Audio
Sensitivity
Course Deviation
Sensitivity
Flag
AGC Characteristics
Selectivity
Standard Deflection
At -103.5 dBm (S+N)/N shall not be less than 6 dB
At –103.5 dBm, deviation output shall not be less than 60% of standard
deflection when a LOC deviation test signal is applied
The VLOC Course Deviation Flag must be flagged:
a) When the level of a standard deviation test signal produces 50% or less of
standard deflection of the deviation indicator
b) In the absence of 150 Hz modulation
c) In the absence of 90 Hz modulation
d) In the absence of both 90 Hz and 150 Hz modulation
e) In the absence of RF
From –99 dBm and –13 dBm input of a Standard VOR Audio Test Signal,
audio output levels shall not vary more than 3 dB
6 dB BW is greater than 9 kHz
69 dB BW is less than 36 kHz
a) With a standard deflection ‘FLY LEFT’ condition (90 Hz dominant), the
output shall be +90 mV ± 9 mV
b) With a standard deflection ‘FLY RIGHT’ condition (150 Hz dominant), the
output shall be -90 mV ± 9 mV
Spurious Response Greater than 60 dB
Centering Accuracy Typical 0 ± 3 mV (Max error 9.9 mV per RTCA DO-195)
Audio Output A minimum 100 mW into a 500 Ω load
Audio Response
Audio Distortion
Less than 6 dB of Variation between 350 and 2500 Hz. In voice mo de , an
ident tone of 1020 Hz shall be attenuated at least 20 dB
The distortion in the receiver audio output shall not exceed 10% at all levels
up to 100 mW
GIA 63 Installation Manual 190-00303-05
Page 1-8 Rev. W
1.4.9 Glideslope Specifications
DRAFT
Table 1-8. GIA 63(X) Glideslope Specifications
Characteristic Specification
Sensitivity
Centering Accuracy 0 ± .0091 ddm or 0 ± 7.8 mV
Selectivity
Standard deflection
Flag
1.4.10 Power Requirements
At –93 dBm, deviation output shall not be less than 60% of standard
deflection when glideslope deviation test signal is applied
6 dB BW is greater than 17 kHz
69 dB BW is less than 132 kHz
a) With a standard deflection ‘FLY DOWN’ condition (90 Hz dominant), the
output shall be -78 mV ± 7.8 mV
b) With a standard deflection ‘FLY UP’ condition (150 Hz dominant), the
output shall be +78 mV ± 7.8 mV
The GS Course Deviation Flag must be flagged:
a) When the level of a standard deviation test signal produces 50% or less of
standard deflection of the deviation indicator
b) In the absence of 150 Hz modulation
c) In the absence of 90 Hz modulation
d) In the absence of both 90 Hz and 150 Hz modulation
e) In the absence of RF
Table 1-9. GIA 63(X) Power Specifications
Characteristic Specification
For P601:
011-00781-0X and 011-01105-0X: 28 Vdc
011-01105-2X/-3X: 14/28 Vdc
011-01105-4X: 28 Vdc
Input Voltage Range
Power Requirements
for P601
(COM Connector)
For P605:
011-00781-0X and 011-01105-0X/-1X/-2X/-3X: 14/28 Vdc
011-01105-4X: 28 Vdc
See the Environmental Qualification Form for details on surge ratings and
minimum/maximum operating voltages.
011-00781-0X and 011-01105-0X/-2X/-3X:
0.3 A max @ 27.5 Vdc (not transmitting);
4.3 A max @ 27.5 Vdc (transmitting)
011-01105-4X:
0.4 A max @ 27.5 Vdc (not transmitting);
4.4 A max @ 27.5 Vdc (transmitting)
011-01105-2X/-3X only:
0.6 A max @ 13.75 Vdc (not transmitting);
6.0 A max @ 13.75 Vdc (transmitting)
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-9
Table 1-9. GIA 63(X) Power Specifications
DRAFT
Characteristic Specification
Superflag Power
Requirements for P605
(Main 2 Connector)
Power Requirements
for P605
(Main 2 Connector)
*Only 011-01105-20 and 011-01105-30 units support both 14 Vdc and 28 Vdc COMs. All
other units
1.4.11 Power Interrupt
Unit Name Unit Part Number Mod Status*
GIA 63
only support 28 Vdc COMs.
Power depends upon loads present on Superflag output pins
(see Sections 4.7.2.1 and 4.10.7)
1.0 A max @ 27.5 Vdc (Without Superflags Active)
2.0 A max @ 13.75 Vdc (Without Superflags Active)
Table 1-10. GIA 63(X) Power Interrupt
Long Term Power Interrupt
Category Per RTCA DO-160**
4 A (200mS)
011-00781-00
0, 1, 2, 3 B (50mS)
1 A (200mS)
011-00781-01
0 B (50mS)
1 A (200mS)
011-01105-00
0 B (50mS)
GIA 63W
GIA 63H 011-01105-30 0 A (200mS)
*Refer to Mod Status Table in front of manual for applicable mod levels.
**Refer to Section 3.8 for Continued Airworthiness. The DO-160 revision used for qualification of each unit is
specified in the applicable environmental qualification form.
011-01105-01 0 A (200mS)
011-01105-20 0 A (200mS)
011-01105-40 0 A (200mS)
GIA 63 Installation Manual 190-00303-05
Page 1-10 Rev. W
1.5 License Requirements
CAUTION
DRAFT
The Telecommunications Act of 1996, effective February 8, 1996, provides the FCC discretion to
eliminate radio station license requirements for aircraft and ships. The GIA 63(X) installation must comply
with current transmitter licensing requirements. To find out the specific details on whether a particular
installation is exempt from licensing, please visit the FCC web site http://wireless.fcc.gov/aviation.
Transmitter Description:
Antenna Characteristics:
Rated Power:
Emission Type:
Frequency of Operation:
If an aircraft license is required, make application for a license on FCC form 404, application for Aircraft
Radio Station License. The FCC also has a fax-on-demand service to provide forms by fax. The GIA 63(X)
owner accepts all responsibility for obtaining the proper licensing before using the transmitter.
International transmitter license procedures vary by country. Contact the local spectrum agency for license
requirements.
The VHF transmitter in this equipment is guaranteed to meet federal communications
commission acceptance over the operating temperature range. Modifications not
expressly approved by Garmin could invalidate the license and make it unlawful to
operate the equipment.
Aviation-band VHF transceiver with 25 and 8.33 kHz channel spacing.
Broad band, 50 ohm, vertically polarized.
16 Watts (28 VDC Operation)
10 Watts (14 VDC Operation; 011-01105-2X and -3X only)
6K00A3E (25 kHz Channel Spacing Mode)
5K6A3E (8.33 kHz Channel Spacing Mode; 011-01105-2X/-3X/-4X
only)
118.000 – 136.992 MHz
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-11
1.6 Certification
DRAFT
The GIA 63 GPS receiver is certified for IFR enroute, terminal, and non-precision approaches. The GIA
63W and the GIA 63H GPS receivers are certified for LNAV/VNAV, LP, and LPV approaches.
The GIA 63(X) has been qualified to RTCA/DO-160 Section 20 RF susceptibility and Section 22 lightning
requirements. Special installation considerations are required, refer to the Environmental Qualification
Form.
The GIA 63(X) meets the requirements for GPS as a Primary Means of Navigation for Oceanic/Remote
Operations per FAA Notice N8110.60.
The GIA 63(X) is eligible for B-RNAV in accordance with AMC 20-4.
Eligible for PRNAV in accordance with PRNAV requirements: JAA Administrative & Guidance Material
Section One: General Part 3: Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and Operational
Approval for Precession RNAV Operations in Designated European Airspace 7.1 Required Functions.
The GIA 63(X) with main software version 7.00 or later and GPS software version 5.0 or later have been
shown to comply with AC 20-165 Appendix 2 and AC 20-138C Appendix 4 and are eligible for use as an
ADS-B Out Position Source meeting the requirements of 14 CFR 91.227 when installed in accordance
with Garmin’s installation instructions.
The conditions and tests required for TSO approval of this article are minimum performance standards. It
is the responsibility of those installing this article either on or within a specific type or class of aircraft to
determine that the aircraft installation conditions are within the TSO standards. TSO articles must have
separate approval for installation in an aircraft. The article may be installed only if performed under 14
CFR part 43 or the applicable airworthiness requirements. At the time of publication, installations of this
TSO approved article are only approved when installed in an aircraft as part of a Garmin Integrated Flight
Deck.
The quantitative safety objective for the VHF Comm radio in the GIA 63W and the GIA 63H is 1 X 10-4
per flight hour for Class I Part 23 Airplanes, and 1 X 10-5 per flight hour for all other Part 23 airplanes and
Parts 25, 27, and 29 aircraft.
GIA 63 Installation Manual 190-00303-05
Page 1-12 Rev. W
1.6.1 GIA 63 TSO/ETSO Compliance
DRAFT
Table 1-11. GIA 63 TSO/ETSO Compliance
Function TSO/ETSO Category
Automatic Pilots
Glideslope
Receiver
Localizer
Receiver
VHF COM
Transmitter
VHF COM
Receiver
VOR Receiver
Flight Director
Equipment
TSO-C9c
ETSO-C9c
TSO-C34e
ETSO-2C34f
TSO-C36e
ETSO-2C36f
TSO-C37d
ETSO-2C37e
TSO-C38d
ETSO-2C38e
TSO-C40c
ETSO-2C40c
TSO-C52b
ETSO-C52b
Class A
Class 3 and 5
Class C and E
Applicable LRU SW Part
Numbers
All
006-B0190-()
except
006-B0190-00
through
006-B0190-19
All
006-B0190-()
except
006-B0190-00
through
006-B0190-04
All
006-B0190-()
except
006-B0190-00
through
006-B0190-04
All
006-B0190-()
except
006-B0190-00
through
006-B0190-04
All
006-B0190-()
except
006-B0190-00
through
006-B0190-04
All
006-B0190-()
except
006-B0190-00
through
006-B0190-04
006-B0190-()
006-B0190-00
006-B0190-19
006-B0083-01
006-B0082-02
006-B0081-0()
except
006-B0081-00
through
006-B0081-04
006-B0081-0()
except
006-B0081-00
through
006-B0081-04
006-B0082-02
All
except
through
All
All
Applicable CLD
Part Numbers
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0053-00
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0053-00
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-13
Table 1-11. GIA 63 TSO/ETSO Compliance
DRAFT
Function TSO/ETSO Category
Ground
Proximity
Warning – Glide
Slope Deviation
Alerting
Equipment
GPS
TAWS
TSO-C92c
TSO-C129a
ETSO-C129a
TSO-C151b Class A and B
ETSO-C151a Class B
Class A1
Applicable LRU SW Part
Numbers
All
006-B0190-()
except
006-B0190-00
through
006-B0190-29
All
006-B0190-()
except
006-B0190-00
through
006-B0190-04
006-B0190-()
006-B0190-00
006-B0190-29
006-B0093-00
006-B0093-01
All
except
through
Applicable CLD
Part Numbers
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
006-C0046-()
006-C0044-()
006-C0047-()
006-C0046-()
006-C0044-()
006-C0047-()
006-C0039-01
GIA 63 Installation Manual 190-00303-05
Page 1-14 Rev. W
1.6.2 GIA 63 TSO/ETSO Deviations
DRAFT
Table 1-12. GIA 63 TSO/ETSO Deviations
TSO/ETSO Deviation
TSO-C9c 1. Garmin was granted a deviation from TSO-C9c to use SAE AS 402B instead of AS-402A.
2. Garmin was granted a deviation from TSO-C9c to use DO-160D instead of specified
environmental tests.
3. Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking the weight
of the unit on the unit. Garmin will provide this information in the installation manual in lieu of marking
on the serial tag. Garmin does not currently list the weight on other avionics units.
4. Garmin was granted a deviation from SAE AS 402B paragraph 4.4.1 to limit autopilot engagement
to attitudes considered safe for the certified aircraft.
5. Garmin was granted a deviation from SAE AS 402B paragraph 4.3.2 to not provide servo effort
indications when the automatic pilot is not engaged.
ETSO-C9c 1. Garmin was granted a deviation from ETSO-C9c to use SAE AS-402B instead of AS-402A.
2. Garmin was granted a deviation from ETSO-C9c to use DO-160D instead of the specified
environmental tests.
3. Garmin was granted a deviation from AS-402B paragraph 4.3.2 to not provide servo effort
indications when the automatic pilot is not engaged.
4. Garmin was granted a deviation from AS-402B paragraph 4.4.1 to limit autopilot engagement to
attitudes considered safe for the certified aircraft.
TSO-C34e 1. Garmin was granted a deviation from TSO-C34e to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
TSO-C36e 1. Garmin was granted a deviation from TSO-C36e to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
TSO-C37d 1. Garmin was granted a deviation from TSO-C37d to use DO-160D Change 3 instead of DO-160B,
TSO-C38d 1. Garmin was granted a deviation from TSO-C38d to use DO-160D Change 3 instead of DO-160B,
TSO-C40c 1. Garmin was granted a deviation from TSO-C40c to use DO-160D Change 3 instead of DO-160B,
TSO-C52b 1. Garmin was granted a deviation from SAE AS 8008 paragraph 3.6 to limit flight director operation
ETSO-C52b 1. Garmin was granted a deviation from AS-8008 paragraph 3.6 to limit flight director operation to
and DO-178B instead of DO-178A.
2. Garmin was granted a deviation from TSO-C37d paragraph (a)(1) to allow using RTCA document
DO-186a Change 2 instead of RTCA document DO-186 to specify minimum performance standards.
3. Garmin was granted a deviation from TSO-C37d by allowing a 6dB reduction of transmitter power
during the Normal Operating Conditions - Emergency Operation Voltage as described in RTCA
document DO-186a paragraph 2.5.13.1 and RTCA document DO-160C paragraph 16.5.2.1.
4. Garmin was granted a deviation from TSO-C37d paragraph (a)(5) to allow 8.33 kHz spacing in
addition to the 25 kHz spacing.
5. Garmin was granted a deviation from TSO-C37d paragraph (b)(1) to allow the marking to call out
8.33 kHz spacing in addition to the 25 kHz spacing.
and DO-178B instead of DO-178A.
2. Garmin was granted a deviation from TSO-C38d paragraph (a)(1) to allow using RTCA document
DO-186a Change 2 instead of RTCA document DO-186 to specify minimum performance standards.
3. Garmin was granted a deviation from TSO-C38d paragraph (a)(5) to allow 8.33 kHz spacing in
addition to the 25 kHz spacing.
and DO-178B instead of DO-178A.
to attitudes considered safe for the certified aircraft.
2. Garmin was granted a deviation from TSO-C52b to use DO-160D instead of DO-160C.
attitudes considered safe for the certified aircraft.
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-15
Table 1-12. GIA 63 TSO/ETSO Deviations
DRAFT
TSO/ETSO Deviation
TSO-C92c 1. Garmin was granted a deviation from TSO-C92c to use DO-160D Change 3 instead of DO-160C.
2. Garmin was granted a deviation from TSO-C92c to not include the version and levels of software
or the modification status of hardware in the appliance number.
TSO-C129a 1. Garmin was granted a deviation from TSO-C129a to use DO-160D Change 3 instead of DO-
160C.
2. Garmin was granted a deviation from TSO-C129a to eliminate the annunciation for pending CDI
scale change 3.0 NM from the FAF.
3. Garmin was granted a deviation from TSO-C129a involving the use of GPS calibrated altitude in
approach mode based on the enclosed TSO deviation request dated August 24, 1994 and the
approval letter dated November 29, 1994.
4. Garmin was granted a deviation from TSO-C129a to extend automatic CDI sensitivity changes to
non-approach mode navigation.
5. Garmin was granted a deviation from TSO-C129a to eliminate the requirement in (a)(3)(xi)1.b.ii to
“alert the pilot of the need to manually insert the barometric pressure”.
6. Garmin was granted a deviation from TSO-C129a to eliminate the requirement in (a)(3)(xv)4.b to
provide a “means to manually identify a satellite that is expected to be unavailable at the destination
(for scheduled maintenance as identified in FAA Notice to Airmen) shall be provided” for the RAIM
prediction process.
7. Garmin was granted a deviation from TSO-C129a to change the requirement in (a)(6)(iii) from
“The navigation data contains all 1’s or 0’s” to “All data bits in subframe 1, 2, or 3 are 0’s”.
8. Garmin was granted a deviation from TSO-C129a to change the requirement in paragraph
(a)(7)(ii) to match the WAAS TSO-C145a and DO-229 requirements for Power input testing.
ETSO-C129a 1. Garmin was granted a deviation from ED-72A 3.2.2.1.f (list item 3) and 3.2.2.4.j.4 to eliminate the
TSO-C151b 1. Garmin was granted a deviation from TSO-C151b 4.a. to mark the unit with the serial number
annunciation for pending CDI scale change 3.0 nm from the FAF.
2. Garmin was granted a deviation from ED-72A 3.2.2.4.j.3 to extend automatic CDI sensitivity
changes for approach mode navigation to non-approach mode navigation as well.
3. Garmin was granted a deviation from ED-72A 3.2.2.1.f (list item 4) and 3.2.2.3.e.4 and 3.2.2.4.j.2
to eliminate the requirement to alert the pilot of the need to manually insert the barometric pressure.
4. Garmin was granted a deviation from ED-72A 3.2.2.3.d.2 to eliminate the requirement to provide a
means to manually identify a satellite that is expected to be unavailable at the destination (for
scheduled maintenance as identified in FAA Notice to Airmen) for the RAIM prediction process.
5. Garmin was granted a deviation from ED-72A 3.1.4.1.c to change the requirement from
“the navigation data contains all 1’s or 0’s” to “all data bits in subframe 1,2, or 3 are 0’s”.
6. Garmin was granted a deviation from ED-72A 4.16.2 to eliminate the requirement for valid position
within 10 seconds of power interrupt for abnormal operating conditions power input tests. For
abnormal operating conditions power input tests, satellite acquisition time of 5 minutes applies.
instead of the date of manufacture.
GIA 63 Installation Manual 190-00303-05
Page 1-16 Rev. W
1.6.3 GIA 63W TSO/ETSO Compliance
DRAFT
Table 1-13. GIA 63W TSO/ETSO Compliance
Function TSO/ETSO Category
Automatic Pilots
Glideslope
Receiver
Localizer
Receiver
TSO-C9c
ETSO-C9c
TSO-C34e
ETSO-2C34f
TSO-C36e
ETSO-2C36f
Class A
Applicable LRU SW Part
Numbers
All
006-B0544-1()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
All
006-B0544-1()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
006-B0544-1()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
006-B0083-0()
except
006-B0083-00
through
006-B0083-01
006-B0082-0()
except
006-B0082-00
through
006-B0082-02
All
All
Applicable CLD
Part Numbers
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0053-0()
except
006-C0053-00
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-17
Table 1-13. GIA 63W TSO/ETSO Compliance
DRAFT
Function TSO/ETSO Category
VOR Receiver
Flight Director
Equipment
Stall Warning
Instruments
TSO-C40c
ETSO-2C40c
TSO-C52b
ETSO-C52b
TSO-C54 Type II
Applicable LRU SW Part
Numbers
All
006-B0544-1()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
006-B0544-1()
006-B0544-4()
006-B0544-B()
006-B0544-BA
006-B0544-BB
006-B0544-4()
006-B0544-B()
006-B0544-BA
006-B0544-BB
006-B0082-0()
except
006-B0082-00
through
006-B0082-02
All
through
and all
except
through
All
and all
except
through
All
Applicable CLD
Part Numbers
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0053-0()
except
006-C0053-00
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
GIA 63 Installation Manual 190-00303-05
Page 1-18 Rev. W
Table 1-13. GIA 63W TSO/ETSO Compliance
DRAFT
Function TSO/ETSO Category
Ground
Proximity
Warning – Glide
Slope Deviation
Alerting
Equipment
Airborne
Navigation
Sensors Using
the Global
Positioning
System
Augmented by
the Wide Area
Augmentation
System*
TAWS
TSO-C92c
ETSO-C92c
TSO-C145a
ETSO-C145
TSO-C151b
ETSO-C151a
TSO-C151b
ETSO-C151b
Class 3
Class B
Class A
and B
Applicable LRU SW Part
Numbers
All
006-B0544-3()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
All
006-B0544-1()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
006-B0544-1()
006-B0544-2()
006-B0544-B()
006-B0544-BA
006-B0544-BB
006-B0544-3()
006-B0544-4()
006-B0544-B()
006-B0544-BA
006-B0544-BB
006-B0339-0()
except
006-B0339-00
through
006-B0339-03
All
through
and all
except
through
All
through
and all
except
through
All
Applicable CLD
Part Numbers
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
190-00303-05 GIA 63 Installation Manual
Rev. W Page 1-19
Table 1-13. GIA 63W TSO/ETSO Compliance
DRAFT
Function TSO/ETSO Category
VHF Radio
Communications
Transceiver
Equipment
*GIA63W ARINC output labels 310 and 311 are not to be used as navigation data per RTCA/DO-229c.
TSO-C169
Equivalent to
ETSO-2C37e
&
ETSO-2C38e
Class 3
and 5
(transmitter)
Class C
and E
(receiver)
Applicable LRU SW Part
Numbers
All
006-B0544-1()
through
006-B0544-4()
and all
006-B0544-B()
except
006-B0544-BA
through
006-B0544-BB
006-B0081-0()
except
006-B0081-00
through
006-B0081-04
All
Applicable CLD
Part Numbers
All
006-C0084-0()
except
006-C0084-00
006-C0072-0()
006-C0085-0()
All
006-C0039-0()
except
006-C0039-00
through
006-C0039-02
GIA 63 Installation Manual 190-00303-05
Page 1-20 Rev. W
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